Research Article
Research on Instability Boundaries of Control Force for Trajectory Correction Projectiles
Table 2
Aerodynamic coefficients of the example projectile.
| Aerodynamic coefficients |
| lift force coefficient | 1.7 | drag force coefficient | 0.13 | Magnus force coefficient derivative | -1.5 | static moment coefficient derivative | 3.8 | Magnus moment coefficient derivative | 0.2 | damping moment coefficient derivative | -8.0 |
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